The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Aug. 14, 2018

Filed:

May. 27, 2014
Applicant:

Aircelle, Gonfreville l'Orcher, FR;

Inventors:

Corentin Hue, Le Havre, FR;

Jérôme Corfa, Cresseveuille, FR;

Assignee:

AIRCELLE, Gonfreville l'orcher, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 29/08 (2006.01); F01D 25/24 (2006.01); B64D 29/06 (2006.01); B64D 33/04 (2006.01); F02K 1/76 (2006.01); B64C 13/28 (2006.01); F16H 25/20 (2006.01);
U.S. Cl.
CPC ...
F01D 25/243 (2013.01); B64D 29/06 (2013.01); B64D 29/08 (2013.01); B64D 33/04 (2013.01); F02K 1/763 (2013.01); B64C 13/28 (2013.01); F05D 2230/80 (2013.01); F16H 2025/2037 (2013.01); F16H 2025/2075 (2013.01); Y02T 50/671 (2013.01);
Abstract

An actuator for an aircraft turbine engine nacelle with a one-piece annular rear part, includes an engine assembly having a nut which is capable of rotating but not of translational movement, and a shaft for turning this nut. The actuator also includes a screw assembly having a screw capable of translational movement without rotating, in mesh with the nut, and a ball joint at one end of this screw intended to be fixed to the annular rear part.


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